Volume I of the report deals with airworthiness assessment and flying qualities evaluation of highly augmented aircraft covered by Parts 23 and 25 of the Federal Aviation Regulations. Particular emphasis has been placed on aircraft with relaxed static stability and on the use of active augmentation systems to achieve the minimum requirement for a level of safety in such aircraft. Significant modifications and expansion to the FAA Engineering Flight Test Guides are detailed. Volume II supports the work of Volume I and provides the more analytically oriented research results of this report. Emphasis is placed on determining the relative similarities and differences between heavily augmented and conventional aircraft. A number of important generic distinctions have been found and are described and explained. (Author)
Flying Qualities of Relaxed Static Stability Aircraft. Volume II. Ramifications of Flight-Essential/Critical Heavily-Augmented Airplane Characteristics on Flying Qualities
1982
126 pages
Report
Keine Angabe
Englisch
Aircraft , Aeronautics , Transport aircraft , Static stability , Airworthiness , Flight control systems , Augmentation , Aerodynamic stability , Center of gravity , Flight testing , Aviation safety , Fuel consumption , Systems analysis , Comparison , Jet transport aircraft , Flying qualities , Relaxed static stability , Augmented flight , Stick fix stability , Stick free stability , Heavy augmented aircraft
Airplane flying qualities specification revision
AIAA | 1968
|Airplane flying qualities specification revision.
AIAA | 1969
|